Trajectory correction scheme based on pulse jet for low speed rolling projectile

Cheng Zhang*, Ying Jun Cao, Shu Xing Yang

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

5 Citations (Scopus)

Abstract

A trajectory correction scheme of pulse jet based on direct force control was brought forward. The starting time selection principle was analyzed. The velocity vector tracing guidance law in horizontal plane was deduced, and the impact point forecast guidance law in the vertical plane was introduced. The fire logic of pulse jets was analyzed, and the control diagram was provided. By numerical simulation, the control scheme was validated. The calculation indicates that the circular probable error reduces to 42 m from 131 m, and the fire accuracy is improved effectively.

Original languageEnglish
Pages (from-to)45-48
Number of pages4
JournalDandao Xuebao/Journal of Ballistics
Volume20
Issue number2
Publication statusPublished - Jun 2008

Keywords

  • Correction
  • Pulse jet
  • Rolling projectile
  • Trajectory

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